| Characteristics of the mission: | |
| Name | Pioneer 11 |
| Nation | United States |
| Objective(s) | Study the interplanetary and planetary magnetic fields; solar wind properties; cosmic rays; transition region of the heliosphere; neutral hydrogen abundance; distribution, size, mass, flux, and velocity of dust particles; Jovian aurorae; Jovian radio waves; the atmospheres of planets and satellites; and the surfaces of Jupiter, Saturn, and some of their satellites. |
| Craft | Pioneer-G |
| Craft – Weight | 259 kg |
| Administration and planning of mission | Ames Research Center - NASA |
| Launch vehicle | Atlas/Centaur/TE364-4 |
| Date and time of launch | 06 April 1973 at 02:11:00 UTC |
| Launched from | Cape Canaveral |
| Scientific instruments/ Technology experiments | |
Pioneer 11 was the second mission to investigate Jupiter and the outer solar system and the first to explore the planet Saturn and its main rings. Pioneer 11 (also called Pioneer G), unlike Pioneer 10 which only visited Jupiter, used Jupiter's mass in a gravitational slingshot to alter its trajectory toward Saturn. It passed close to Saturn and then it followed an escape trajectory from the solar system.
The spacecraft was launched from Cape Canaveral on April 6, 1973. It is 2.9 meters long and has a 2.74-meter-diameter high-gain antenna, topped with a medium-gain antenna. A low-gain, omnidirectional antenna is mounted below the high-gain dish. The spacecraft contains two radioisotope thermoelectric generators (RTGs), which generated 144 W at Jupiter, but had decreased to 100 W by the time it reached Saturn. There were three reference sensors: a star (Canopus) sensor, and two Sun sensors. Attitude position could be calculated from the reference direction to Earth and Sun, with the known direction to Canopus as backup. Pioneer 11's star sensor gain and threshold settings were modified, based on experience gained from the settings used on Pioneer 10. Three pairs of rocket thrusters provided spin-axis control (maintained at 4.8 rpm) and change the spacecraft's velocity. The thrusters could be either fired steadily or pulsed, by command.
Instruments studied the interplanetary and planetary magnetic fields; solar wind properties; cosmic rays; the transition region of the heliosphere; neutral hydrogen abundance; distribution, size, mass, flux, and velocity of dust particles; Jovian aurorae; Jovian radio waves; the atmospheres of planets and satellites; and the surfaces of Jupiter, Saturn, and some of their satellites. The instruments carried for these experiments were a magnetometer, a plasma analyzer (for solar wind), a charged-particle detector, an ion detector, non-imaging telescopes with overlapping fields of view to detect sunlight reflected from passing meteoroids, sealed pressurized cells of argon and nitrogen gas for measuring penetration of meteoroids, an ultraviolet photometer, an infrared radiometer, and an imaging photopolarimeter, which produced photographs and measured their polarization. Further scientific information was obtained from celestial mechanics and occultation phenomena.
(By this time Voyager 1 and Voyager 2 had already passed Jupiter and were also en route to Saturn.) It was decided to target Pioneer 11 to pass through the Saturn ring plane at the same position that the soon-to-come Voyager probe would use in order to test the route before Voyager arrived. If there were faint ring particles that could damage a probe in that area, mission planners felt it was better to learn about it via Pioneer. Thus, Pioneer 11 was acting as a "pioneer" in a true sense of the word. (If danger was detected, then the Voyager probes could be rerouted further away from the rings, but missing the opportunity to visit Uranus and Neptune in the process.)
Instruments located two previously undiscovered small moons and an additional ring, charted Saturn's magnetosphere and magnetic field and found its planet-size moon, Titan, to be too cold for life. Hurtling underneath the ring plane, Pioneer 11 sent back amazing pictures of Saturn's rings. The rings, which normally seem bright when observed from Earth, appeared dark in the Pioneer pictures, and the dark gaps in the rings seen from Earth appeared as bright rings.
December 2, 1974 Flyby of Jupiter.
September 1, 1979 Flyby of Saturn.
February, 1985 Instrument power sharing began due to declining generator power output.
September 30, 1995 Routine daily mission operations stopped. Pioneer 11 is 6.5 billion km from Earth.
November, 1995 Last communication with Pioneer 11.
Analysis of the radio tracking data from the Pioneer 10 and 11 spacecraft at distances between 20–70 AU from the Sun has consistently indicated the presence of an anomalous, small Doppler frequency drift. The drift can be interpreted as being due to a constant acceleration of (8.74 ± 1.33) × 10−10 m/s2 directed towards the Sun. Although it is suspected that there is a systematic origin to the effect, none has been found. As a result, the nature of this anomaly has become of growing interest.
Jupiter spacecraft | Pioneer program | Saturn spacecraft
Pioneer 11 | Pioneer 11 | Pioneer 11 | Pioneer 11 | 파이어니어 11호 | Pioneer 11 | Pioneer–11 | パイオニア11号 | Pioneer 11 | Pioneer 11 | Пионер-11 | Pioneer 11 | Pioneer 11 | Pioneer 11 | 先驱者11号
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